View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 25860U 99039A 25194.39757227 .00000469 00000-0 69225-4 0 9991
2 25860 97.9821 251.2331 0001748 76.0838 284.0568 14.79838237399082
| Epoch (UTC): | 13 July 2025 09:32:30 |
| Eccentricity: | 0.0001748 |
| inclination: | 97.9821° |
| perigee height: | 628 km |
| apogee height: | 631 km |
| right ascension of ascending node: | 251.2331° |
| argument of perigee: | 76.0838° |
| revolutions per day: | 14.79838237 |
| mean anomaly at epoch: | 284.0568° |
| orbit number at epoch: | 39908 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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